TY - BOOK ID - 135099981 TI - Explicit finite element modeling of multilayer composite fabric for gas turbine engine containment systems : final report. PY - 2004 PB - Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research, DB - UniCat KW - Aircraft gas-turbines KW - Airplanes KW - Fibrous composites KW - Ballistic fabrics KW - Finite element method. KW - Safety measures KW - Testing. KW - Turbine-propeller engines KW - Impact testing. UR - https://www.unicat.be/uniCat?func=search&query=sysid:135099981 AB - ER -